CA2598532C - Aube de rotor d'une turbomachine - Google Patents

Aube de rotor d'une turbomachine Download PDF

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Publication number
CA2598532C
CA2598532C CA2598532A CA2598532A CA2598532C CA 2598532 C CA2598532 C CA 2598532C CA 2598532 A CA2598532 A CA 2598532A CA 2598532 A CA2598532 A CA 2598532A CA 2598532 C CA2598532 C CA 2598532C
Authority
CA
Canada
Prior art keywords
cleat
flange
disc
disk
face
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CA2598532A
Other languages
English (en)
French (fr)
Other versions
CA2598532A1 (fr
Inventor
Yvon Cloarec
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SNECMA SAS filed Critical SNECMA SAS
Publication of CA2598532A1 publication Critical patent/CA2598532A1/fr
Application granted granted Critical
Publication of CA2598532C publication Critical patent/CA2598532C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CA2598532A 2006-08-25 2007-08-22 Aube de rotor d'une turbomachine Active CA2598532C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0607510 2006-08-25
FR0607510A FR2905139B1 (fr) 2006-08-25 2006-08-25 Aube de rotor d'une turbomachine

Publications (2)

Publication Number Publication Date
CA2598532A1 CA2598532A1 (fr) 2008-02-25
CA2598532C true CA2598532C (fr) 2014-05-27

Family

ID=37507783

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2598532A Active CA2598532C (fr) 2006-08-25 2007-08-22 Aube de rotor d'une turbomachine

Country Status (6)

Country Link
US (1) US7850430B2 (de)
EP (1) EP1895103B1 (de)
CA (1) CA2598532C (de)
DE (1) DE602007011169D1 (de)
FR (1) FR2905139B1 (de)
RU (1) RU2455496C2 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2929660B1 (fr) * 2008-04-07 2012-11-16 Snecma Dispositif anti-usure pour rotor de turbomachine, bouchon formant dispositif anti-usure et rotor de compresseur de moteur a turbine a gaz comportant un bouchon anti-usure
US20100254807A1 (en) * 2009-04-07 2010-10-07 Honeywell International Inc. Turbine rotor seal plate with integral flow discourager
US8007230B2 (en) * 2010-01-05 2011-08-30 General Electric Company Turbine seal plate assembly
US8961141B2 (en) 2011-08-29 2015-02-24 United Technologies Corporation Axial retention system for a bladed rotor with multiple blade types
JP2018104251A (ja) * 2016-12-28 2018-07-05 パナソニックＩｐマネジメント株式会社 炭素・金属複合材とそれが添加されたゴム組成物および樹脂組成物
FR3091719B1 (fr) 2019-01-15 2021-02-12 Safran Aircraft Engines secteur de flasque d’etancheite de disque de rotor
FR3092861B1 (fr) * 2019-02-18 2023-02-10 Safran Aircraft Engines Ensemble de turbomachine comportant un taquet sur un jonc d'etancheite
FR3093131B1 (fr) * 2019-02-22 2021-10-01 Safran Aircraft Engines Ensemble pour turbomachine
FR3095234B1 (fr) * 2019-04-19 2021-07-09 Safran Aircraft Engines Ensemble de turbomachine comprenant un dispositif de limitation de temperature pour fond d’alveole non refroidi
FR3109604B1 (fr) 2020-04-27 2022-08-26 Safran Aircraft Engines Roue aubagee a performances d’etancheite et de retention des aubes ameliorees

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB699582A (en) * 1950-11-14 1953-11-11 Rolls Royce Improvements in or relating to gas-turbine engines
US3853425A (en) * 1973-09-07 1974-12-10 Westinghouse Electric Corp Turbine rotor blade cooling and sealing system
FR2324873A1 (fr) * 1975-09-17 1977-04-15 Snecma Perfectionnements aux flasques de rotors de turbomachines
US4453890A (en) * 1981-06-18 1984-06-12 General Electric Company Blading system for a gas turbine engine
FR2535793B1 (fr) * 1982-11-08 1987-04-10 Snecma Dispositif de verrouillage axial d'aubes de soufflante
FR2700807B1 (fr) * 1993-01-27 1995-03-03 Snecma Système de rétention et d'étanchéité d'aubes engagées dans des brochages axiaux d'un disque de rotor.
GB2307279B (en) * 1995-11-14 1999-11-17 Rolls Royce Plc A gas turbine engine
WO1997049921A1 (de) * 1996-06-21 1997-12-31 Siemens Aktiengesellschaft Rotor für eine turbomaschine mit in nuten anbringbaren schaufeln sowie schaufel für einen rotor
RU2238412C1 (ru) * 2003-04-28 2004-10-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Рабочее колесо турбины
US7530791B2 (en) * 2005-12-22 2009-05-12 Pratt & Whitney Canada Corp. Turbine blade retaining apparatus

Also Published As

Publication number Publication date
EP1895103A3 (de) 2009-01-21
EP1895103A2 (de) 2008-03-05
EP1895103B1 (de) 2010-12-15
FR2905139A1 (fr) 2008-02-29
RU2455496C2 (ru) 2012-07-10
US20080050245A1 (en) 2008-02-28
FR2905139B1 (fr) 2012-09-28
US7850430B2 (en) 2010-12-14
CA2598532A1 (fr) 2008-02-25
RU2007132178A (ru) 2009-02-27
DE602007011169D1 (de) 2011-01-27

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